Structural feedback linearization based on nonlinearities rejection

L. A. Blas; M. Bonilla; M. Malabre; V. Azhmyakov; S. Salazar

doi:10.1016/j.ifacol.2017.08.090

Structural feedback linearization based on nonlinearities rejection

L. A. Blas, M. Bonilla, M. Malabre, V. Azhmyakov, S. Salazar

Grupo de Investigación en Modelación y Computación Científica

Producción científica: Contribución a una revista › Artículo › revisión exhaustiva

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© 2017 In this paper, a structural feedback linearization technique is proposed. This is a quite simple and effective linear control scheme based on failure detection techniques. Our proposed linear control approach is intended to reject the nonlinearities, which are treated as failure signals affecting the systems dynamics. The proposed control methodology is illustrated via the attitude control of a quadrotor in hover flying.

Idioma original	Inglés estadounidense
Páginas (desde-hasta)	922-927
Número de páginas	6
Publicación	IFAC-PapersOnLine
DOI	https://doi.org/10.1016/j.ifacol.2017.08.090
Estado	Publicada - 1 jul. 2017

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10.1016/j.ifacol.2017.08.090

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@article{715827bb55c1439a80eafada71fb94e4,

title = "Structural feedback linearization based on nonlinearities rejection",

abstract = "{\textcopyright} 2017 In this paper, a structural feedback linearization technique is proposed. This is a quite simple and effective linear control scheme based on failure detection techniques. Our proposed linear control approach is intended to reject the nonlinearities, which are treated as failure signals affecting the systems dynamics. The proposed control methodology is illustrated via the attitude control of a quadrotor in hover flying.",

author = "Blas, {L. A.} and M. Bonilla and M. Malabre and V. Azhmyakov and S. Salazar",

year = "2017",

month = jul,

day = "1",

doi = "10.1016/j.ifacol.2017.08.090",

language = "American English",

pages = "922--927",

journal = "IFAC-PapersOnLine",

issn = "2405-8963",

publisher = "IFAC Secretariat",

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TY - JOUR

T1 - Structural feedback linearization based on nonlinearities rejection

AU - Blas, L. A.

AU - Bonilla, M.

AU - Malabre, M.

AU - Azhmyakov, V.

AU - Salazar, S.

PY - 2017/7/1

Y1 - 2017/7/1

N2 - © 2017 In this paper, a structural feedback linearization technique is proposed. This is a quite simple and effective linear control scheme based on failure detection techniques. Our proposed linear control approach is intended to reject the nonlinearities, which are treated as failure signals affecting the systems dynamics. The proposed control methodology is illustrated via the attitude control of a quadrotor in hover flying.

AB - © 2017 In this paper, a structural feedback linearization technique is proposed. This is a quite simple and effective linear control scheme based on failure detection techniques. Our proposed linear control approach is intended to reject the nonlinearities, which are treated as failure signals affecting the systems dynamics. The proposed control methodology is illustrated via the attitude control of a quadrotor in hover flying.

U2 - 10.1016/j.ifacol.2017.08.090

DO - 10.1016/j.ifacol.2017.08.090

M3 - Article

SN - 2405-8963

SP - 922

EP - 927

JO - IFAC-PapersOnLine

JF - IFAC-PapersOnLine

ER -

Structural feedback linearization based on nonlinearities rejection

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